Ir al contenido (pulsa Retorno)

Universitat Politècnica de Catalunya

    • Català
    • Castellano
    • English
    • LoginRegisterLog in (no UPC users)
  • mailContact Us
  • world English 
    • Català
    • Castellano
    • English
  • userLogin   
      LoginRegisterLog in (no UPC users)

UPCommons. Global access to UPC knowledge

Banner header
66.439 UPC academic works
You are here:
View Item 
  •   DSpace Home
  • Treballs acadèmics
  • Màsters oficials
  • Master's degree in Aerospace Science and Technology - MAST (Pla 2015)
  • View Item
  •   DSpace Home
  • Treballs acadèmics
  • Màsters oficials
  • Master's degree in Aerospace Science and Technology - MAST (Pla 2015)
  • View Item
JavaScript is disabled for your browser. Some features of this site may not work without it.

Design and Implementation of a femto-satellite technology demonstrator

Thumbnail
View/Open
memoria.pdf (1,838Mb)
  View Usage Statistics
  LA Referencia / Recolecta stats
Cita com:
hdl:2099.1/12441

Show full item record
Kravchenko, Victor
Tutor / directorTristancho Martínez, JoshuaMés informació
Document typeMaster thesis
Date2011-07-05
Rights accessOpen Access
Attribution-NonCommercial-ShareAlike 3.0 Spain
Except where otherwise noted, content on this work is licensed under a Creative Commons license : Attribution-NonCommercial-ShareAlike 3.0 Spain
Abstract
The present work is aimed to demonstrate the development and implementation of a scalable femto-satellite technology demonstrator, experimentation and development platform in order to practically prove the possibility of meeting the N-Prize competition requirements as well as introducing some possible scientific applications of a femto-satellite as a satellite-on-a-board spacecraft. In order to achieve these goals the low-cost low-power self-sufficient platform with communication, data processing position determination and keeping abilities was designed and implemented. A set of subsystem qualification tests was designed and performed in order to obtain numerical results and calls for the future studies. The ability to meet the general space qualification and particular N-Prize competition-related requirements was studied and the overall conclusions were stated.
Description
Este estudio esta destinado al dise?o, construccion y prueba de una plataforma llamada Aerial Wireless Inertial Platform (AWIP) que tiene capacidad de comunicacion inalambrica, altas prestaciones y fiabilidad, sensor de actitud y velocidad de giro, bajo consumo, bajo coste, un alto nivel de integracion y bajo peso. Esta plataforma tiene muchas aplicaciones pero la mayor restriccion es debido a las exigencias del entorno para el espacio que debe reunir. La AWIP debe ser dise?ada como un demostrador multi-funcional para aplicaciones de Femto-satelites asi como vehiculos no tripulados UAV en enjambre, nube de sensores, etc. En esta Tesis, se estudia la posibilidad de aplicarlo a un Femto-satelite para una mision basica en LEO y que tiene como finalidad probar el modelo escalable para misiones de complejidad aumentada. El lugar de investigacion sera en los laboratorios aeronauticos, como el tunel de viento, con un bajo coste y creando herramientas SMT o Surface Mount Technology.
SubjectsMicrospacecraft, Astronautics, Astronàutica
URIhttp://hdl.handle.net/2099.1/12441
Collections
  • Màsters oficials - Master's degree in Aerospace Science and Technology - MAST (Pla 2015) [160]
  View Usage Statistics

Show full item record

FilesDescriptionSizeFormatView
memoria.pdf1,838MbPDFView/Open

Browse

This CollectionBy Issue DateAuthorsOther contributionsTitlesSubjectsThis repositoryCommunities & CollectionsBy Issue DateAuthorsOther contributionsTitlesSubjects

© UPC Obrir en finestra nova . Servei de Biblioteques, Publicacions i Arxius

info.biblioteques@upc.edu

  • About This Repository
  • Contact Us
  • Send Feedback
  • Privacy Settings
  • Inici de la pàgina